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LEMUR-2-SEJONG-3

In orbit NORAD 68482 DXKF-1992-5459-8138-9868

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-SEJONG-3
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
582.50 km
Apogee
585.48 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6962.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 68482U 26067BU  26284.12623160  .00002856  00000-0  27658-3 0  9994
2 68482 97.7718 240.9825 0002140 203.0536 157.0588 14.93518003 29037
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 06:46:43 LEMUR-2-SEJONG-3
NORAD 68482
COSMOS 2251 DEB
NORAD 38208
1.476 7.49 1.8e-06
2026-10-13 15:45:36 DEIMOS-2
NORAD 40013
LEMUR-2-SEJONG-3
NORAD 68482
0.889 10.27 4.3e-06
2026-10-13 16:33:50 DEIMOS-2
NORAD 40013
LEMUR-2-SEJONG-3
NORAD 68482
4.833 10.29 1.5e-07
2026-10-14 00:32:35 LEMUR-2-SEJONG-3
NORAD 68482
FENGYUN 1C DEB
NORAD 32432
4.197 9.37 2.0e-07
2026-10-14 03:48:30 LEMUR-2-SEJONG-3
NORAD 68482
PEARL-1A
NORAD 68990
4.489 7.72 1.9e-07
2026-10-14 05:19:23 LEMUR-2-SEJONG-3
NORAD 68482
CZ-6A DEB
NORAD 54576
2.855 13.43 3.0e-07
2026-10-14 17:25:06 LEMUR-2-SEJONG-3
NORAD 68482
CZ-6A DEB
NORAD 61455
3.651 13.94 1.6e-07
2026-10-14 18:34:04 AAC-AIS-SAT2
NORAD 56996
LEMUR-2-SEJONG-3
NORAD 68482
2.566 14.99 2.4e-07
2026-10-15 16:46:21 LEMUR-2-SEJONG-3
NORAD 68482
N1-ATLAS
NORAD 68501
4.708 0.04 2.0e-07
2026-10-15 17:34:34 LEMUR-2-SEJONG-3
NORAD 68482
VINDLER 2.2
NORAD 68484
4.146 0.08 2.6e-07
2026-10-15 19:10:51 LEMUR-2-SEJONG-3
NORAD 68482
VINDLER 2.3
NORAD 68486
4.997 0.04 1.8e-07
2026-10-15 23:03:29 IRIDE-MS2-HEO-3
NORAD 64568
LEMUR-2-SEJONG-3
NORAD 68482
3.549 14.66 1.4e-07
2026-10-16 00:22:25 SHIYAN-30 02
NORAD 65852
LEMUR-2-SEJONG-3
NORAD 68482
3.750 7.97 2.7e-07
2026-10-16 01:01:33 LEMUR-2-SEJONG-3
NORAD 68482
FENGYUN 1C DEB
NORAD 32137
2.704 14.88 2.3e-07
2026-10-16 20:07:31 LEMUR-2-SEJONG-3
NORAD 68482
IRIDE-MS2-HEO-13
NORAD 68985
3.570 7.69 3.0e-07
2026-10-16 23:12:08 LEMUR-2-SEJONG-3
NORAD 68482
CZ-4B DEB
NORAD 26262
2.678 14.44 2.7e-07
2026-10-17 02:07:19 SHIYAN-30 01
NORAD 65851
LEMUR-2-SEJONG-3
NORAD 68482
3.809 7.89 2.6e-07
2026-10-17 12:33:51 SHIYAN-30 03
NORAD 68139
LEMUR-2-SEJONG-3
NORAD 68482
4.912 7.91 1.6e-07
2026-10-17 16:08:26 LEMUR-2-SEJONG-3
NORAD 68482
COSMOS 2221
NORAD 22236
4.357 15.10 7.8e-08

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite